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MIL-0-11585B — OUTBOARD ENGINE

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

MIL-0-11585B: OUTBOARD ENGINE.

The OUTBOARD ENGINE is a the manufacturer industrial component. Key specifications include fuel_type: GASOLINE, cooling_type: DIRECT WATER, starting_method: MANUAL, features_provided: INTEGRAL REVERSE GEAR AND GEAR REDUCTION, reduction_gear_ratio: 12TO21, propeller_blade_pitch: 12.500 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 2805-00-294-3598, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.

Verify compatibility with your specific system configuration before ordering.

WHERE IT FITS
MIL-0-11585B
NSN: 2805-00-294-3598
FSC: 2805 — Gasoline Reciprocating Engines, Except Aircraft; and Components
CAGE: 81349 — MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
SPECIFICATIONS
fuel_typeGASOLINE
cooling_typeDIRECT WATER
starting_methodMANUAL
cylinder_quantity2
features_providedINTEGRAL REVERSE GEAR AND GEAR REDUCTION
reduction_gear_ratio12TO21
propeller_blade_pitch12.500 INCHES NOMINAL IN
propeller_blade_diameter11.000 INCHES NOMINAL IN
propeller_blade_quantity3
propeller_attachment_methodKEY OR LOCKNUT
NSN2805-00-294-3598
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available OUTBOARD ENGINE TITLE COMPONENT PN MIL-0-11585B MFR OUTBOARD ENGINE
KEY FEATURES
•
COOLING TYPE: DIRECT WATER
•
PROPELLER BLADE DIAMETER: 11.000 INCHES NOMINAL IN
•
PROPELLER BLADE QUANTITY: 3
•
PROPELLER ATTACHMENT METHOD: KEY OR LOCKNUT
•
REDUCTION GEAR RATIO: 12TO21
•
FUEL TYPE: GASOLINE
•
FEATURES PROVIDED: INTEGRAL REVERSE GEAR AND GEAR REDUCTION
•
STARTING METHOD: MANUAL
TECHNICAL CHARACTERISTICS
COOLING TYPEDIRECT WATER
PROPELLER BLADE DIAMETER11.000 INCHES NOMINAL IN
PROPELLER BLADE QUANTITY3
PROPELLER ATTACHMENT METHODKEY OR LOCKNUT
REDUCTION GEAR RATIO12TO21
FUEL TYPEGASOLINE
FEATURES PROVIDEDINTEGRAL REVERSE GEAR AND GEAR REDUCTION
STARTING METHODMANUAL
SPECIAL FEATURESHORIZONTALLY OPPOSED, 2.875 IN. BORE DIA, 2.750 IN. STROKE LG, CARBURETOR FUEL INDUCTION, MAGNETO IGNITION, AUTOMATIC REWIND STARTER ROPE, ELECTROMAGNETIC INTERFERENCE SUPPRESSION PROVIDED, POWER TRANSMITTED FROM VERTICAL DRIVE SHAFT THROUGH HEAVY DUTY REDUCTION GEARS TO HORIZONTAL PROPELLER SHAFT, FORWARD AND REVERSE OPERATION, 1 SPEED FORWARD, 1 SPEED REVERSE, W/SEPARATE FUEL TANK, 6 GALLON CAPACITY, W/CARRYING HANDLE AND FUEL GAGE, W/CHEST PROVIDED W/SKIDS IN
CYLINDER QUANTITY2
OTHER ITEMS IN FSC 2805 — Gasoline Reciprocating Engines, Except Aircraft; and Components
Items in the same Federal Supply class. No interchangeability or substitution relationship is implied.
2805-00-000-4022 2805-00-001-0029 2805-00-001-3527 2805-00-001-3844 2805-00-001-3854 2805-00-001-6154 2805-00-001-6164 2805-00-001-6575
SUBSTITUTES & CROSS-REFERENCES 1
RDM12Reference document
Same NSN cross-reference
Reference document — Secondary reference
LIFECYCLE
NSN statusActive· U.S. Government catalog
Acquisition advice: Terminal item — stock exhausted; no further procurementNo demilitarization required
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FREQUENTLY ASKED QUESTIONS
What is MIL-0-11585B?
MIL-0-11585B is a OUTBOARD ENGINE.
What parts can replace MIL-0-11585B?
There is 1 known substitute for MIL-0-11585B: RDM12. Substitute compatibility should be verified for your specific system.
What is the NSN for MIL-0-11585B?
MIL-0-11585B is cataloged in the U.S. Government catalog under NSN 2805-00-294-3598. This indicates validated use in U.S. government and defense supply chains.
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